双铰翼的评价

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Shun Watanabe, S. Sunada, K. Yamaguchi
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引用次数: 1

摘要

在恒定升力系数和恒定飞行速度条件下,采用涡点阵法分析了两种模拟鸟类滑翔飞行的机翼几何形状在改变关节位置和关节角度时的升阻比和根部弯矩。一种几何形状是,有时被称为海鸥翼,它具有二面体的内翼和水平的外翼,称为“DH翼”。相反,另一种几何形状是内翼为水平,外翼为四面体的下垂翼,称为“HA翼”。当四面体外翼结合部靠近翼尖且棱角较大时,HA翼的升阻比增大,而当四面体外翼结合部靠近翼根且棱角较大时,HA翼的根部弯矩减小。相比之下,DH翼没有结合关节位置和关节角度来提高升阻比,研究发现,与DH翼相比,HA翼有效地降低了根部弯矩和升阻比。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Evaluation of Two-Hinged Wings
Two types of wing geometries imitating wings of birds in gliding fl ight are analyzed with the vortex lattice method in terms of lift-drag ratio and root bending moment while varying the joint positions and joint angles under the constant lift coe ffi cient and constant fl ight velocity conditions. One geometry is, what is sometimes called, a gull wing which has a dihedral inner wing and horizontal outer wing, named “ DH wing. ” On the contrary, the other geometry is a drooped wing which has a horizontal inner wing and anhedral outer wing, named “ HA wing. ” The lift-drag ratio of the HA wing becomes larger when the joint of the anhedral outer wing is closer to the wing tip with a larger anhedral angle, while the root bending moment of the HA wing becomes smaller when the joint of the anhedral outer wing is closer to the wing root with a larger anhedral angle. In contrast, the DH wing has no combination of a joint position and joint angle to improve the lift-drag ratio, and it is found that the HA wing e ff ectively contributes to the reduction of the root bending moment and the lift-drag ratio compared with the DH wing.
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来源期刊
CiteScore
1.80
自引率
0.00%
发文量
18
审稿时长
>12 weeks
期刊介绍: Information not localized
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